Process for Structurally Joining Modular Hollow Columns or Rods Generically Elongated in Shape and the Product Obtained

ABSTRACT

The invention is a new process for the production of a hollow structural column or rod in polymers, obtained by assembling modules having shorter length, comprising two or more elongated modules, each one provided with male-female truncated cone-shaped terminal parts ( 56, 56 ), wherein the inner surface of the “female” terminal part ( 56 ) has a taper angle that is identical to the taper angle of the outer surface of the “male” terminal part ( 53 ), and comprising the following steps: aligning said hollow modules; preparing said male and female terminal parts with adhesive for glueing and insertion in the terminal part of the adjacent, aligned module; applying, preferably at the ends, an axial compression device, so that on compression of the ends of the rod made up of said modules each external male tapering surface adheres to and exerts a suitable pressure on the internal female tapering surface of the adjacent module during the structural joining and glueing of the terminal parts and the polymerisation of the adhesive.

TECHNICAL FIELD

The present patent concerns the production of hollow columns or rods in polymeric materials, reinforced with fibres or not, to be used for any application where a support column is required, for example, but not exclusively, as support for electric lines, lighting installations, overhead platforms, and in particular it concerns the production of masts in resin reinforced with fibres for sailboats. The present patent describes a method suitable for structurally joining elongated modules, constituting just a section of the whole length of the column or rod and therefore easy to transport. Said modules can be equal to or different from one another and they can be produced in series, at the same time maintaining the adaptability of the entire column or rod to the needs of any specific supply. Said modules can be produced with any known technology for the manufacture of products in resin reinforced with fibres, even if said technology should not be applicable to the entire column or rod due to its overall dimensions.

GENERAL NOTES ON THE PRODUCTION OF COMPOSITE MATERIALS

Many objects are made of composite material consisting of a thermosetting resin, usually an epoxy resin, reinforced with fibres, usually carbon or glass or aramidic fibres. The layers of fibre, impregnated by hand or pre-impregnated with resin, are arranged on the internal surface of a mould. The resin is then heat-polymerised, in such a way as to obtain a solid whose external shape is identical to the internal surface of the mould. To obtain composite materials with excellent mechanical properties it is fundamental to eliminate any air that may be included between the various layers of fibre and to make these layers of fibres adhere strongly to one another.

To achieve this purpose, the mould with the laminated layers of fibres and resin is enclosed in a bag which is then placed in an autoclave.

The bag containing the mould and the laminate is connected to a vacuum pump, while pressure in the autoclave is brought to a suitable value.

As a result the laminate of fibres and resin is crushed against the mould and at the same time any air that may have been trapped between the fibres and the resin is extracted. To obtain materials with excellent mechanical properties it is of fundamental importance to eliminate the air which remains trapped between the various reinforcing layers during lamination.

It is also fundamental to place the various layers of fibres in close contact with one another.

These results are obtained by applying high pressures, up to 6˜7 bars. Furthermore, many resins require high temperatures to polymerize correctly. In the case of very long structures, like the masts of sailboats, the cost of the autoclave necessary to obtain optimal pressures and temperatures is very high. Furthermore, the moulds necessary to make masts for sailboats are large and heavy and consequently costly and difficult to handle. Another problem is represented by the inspection of the fibres during the lamination of very long pieces and by the positioning of any internal components.

AIM OF THE INVENTION

To overcome all these drawbacks, a new process for the production of hollow rods in modules has been studied.

The aim of the new process is to obtain elongated hollow objects, in resin reinforced with fibres, treated/cured at high pressure and temperature, typically in autoclave.

Another aim of the new process is to obtain long objects starting from shorter modules produced with various technologies and materials, and joined using a reliable method that doesn't affect the structural characteristics required.

Another aim of the process is to obtain elongated hollow objects with internal cross reinforcements that increase the stability of their walls.

A further aim of the process is to obtain long objects, starting from short modules that are easy to transport and that can be joined without using costly and cumbersome equipment, even away from the place where the single modules were produced.

A further aim of the process is to obtain modules that can be easily and economically transported anywhere to make up a longer object, which would be difficult to transport, without using specific equipment.

Another aim of the process is to obtain modules that can be produced in series and assembled according to different combinations, thus allowing the customization of the column or rod, for example by varying its length, or the shape of its ends, or installing couplings or supports in different positions, with no need to carry out any tools or equipment specifically for this purpose.

These and other aims, direct and complementary, are achieved by the new process for the production of modular columns or rods.

DESCRIPTION OF THE INVENTION

The particular application described herein is suitable for the production of masts for sailboats, but it may be used to produce posts for road lights and for electric energy, for platform supports, for columns and in general for any elongated hollow structure, with any cross section (circular, elliptic, with an aerodynamic profile, etc.) and with any length. The invention makes it possible to carry out and transport this type of structure in separate modules, unlike other processes that require the construction of a single piece. The special feature of the invention lies in that it ensures a more precise quality control on the joins between the different modules compared to traditional methods. Thanks to the joining method proposed, the glueing areas constitute a local reinforcement for the column in its whole, instead of an area of potential structural weakness.

The new process makes it possible to produce modular elongated hollow structures, in resin reinforced with fibres and polymerised at high pressure. The advantage offered by this method is represented by the fact that it allows components with reduced length to be joined in a controlled way, without penalizing the structural characteristics of the assembly, to obtain rods having the desired length. The high-pressure treatment/curing of masts made of composite material in autoclave offers considerable advantages compared to the treatment/curing at atmospheric pressure or only with the bag under vacuum and the method described herein allows said treatment/curing process to be carried out in autoclaves with limited length, not expressly meant for treating/curing masts, also benefiting from a method for joining the modules where the structural resistance of the finished mast isn't penalized, but, rather, a local reinforcement that reduces the instability of the walls is created.

In the variant described herein, in fact, the advantage of glueing under pressure surfaces that are perfectly coupled is combined with the presence of transversal diaphragms that limit deformations that are perpendicular to the surface of the wall, thus reducing the risk of local instability of the wall itself. These diaphragms, which cannot be obtained in a monolithic tubular structure, are in any case difficult to insert even in a normal tubular structure constituted by two elements joined in the middle. With the proposed method, instead, the presence of these diaphragms is automatic, if the modules are carried out with a perimetral rib at one end.

With the new process separate modules can be produced, whose length can be chosen according to the length of the autoclave to be used and to the characteristics of the column to be obtained by joining them. These modules can be equal to one another, in which case, once joined, they will constitute a tubular shape with substantially constant cross section, but can also have different features, for example tapering parts for the mast ends, different types of inserts and couplings for the installation of accessories, terminal elements for the base or the top of the mast. It is also possible to produce without difficulties a totally or partially sealed tight module, or a module containing a foamed material, in order to achieve a reserve buoyancy that is useful to prevent sailboats from overturning.

For a partially serialized production of masts for sailboats, few moulds with reduced dimensions and limited costs can be prepared, with which it is possible to obtain masts having different lengths and characteristics, according to the customer's needs, and equipped with all the complements that usually must be installed later on.

The fundamental feature that ensures that the join is structurally and economically advantageous is the shape of the terminal part of the modules.

The terminal parts of the modules must be in the shape of a truncated cone, with dimensions suitable for introducing one terminal part into the other. In this way, an axial compression, which can be easily obtained by using a traction cable or rod with threaded ends that is made slide inside the mast, is converted into a pressure perpendicular to the adjacent surfaces of the terminal parts in the shape of truncated cones.

This pressure can be easily controlled by controlling traction on the inner cable, for example using a torque wrench on nuts screwed to the threaded ends of the cable and acting on suitable retaining plates at the ends of the mast.

The pressure on the walls of the truncated cone-shaped terminal parts of the modules can thus be adjusted according to the characteristics of the adhesive used for joining the modules, thus allowing said adhesive to be perfectly treated/cured.

The pressure also allows any excess adhesive or any air bubbles to be eliminated. The excessive thickness of the adhesive and the presence of air bubbles inside it are the two main sources of defects in the glued joins and are normally avoided by applying high pressures on the surfaces to be joined. The method proposed herein ensures easy application of pressure on the surfaces to be glued together, with no need to use costly equipment or to adopt complex solutions.

Another effect of the pressure on the truncated cone-shaped terminal parts of the modules is that they are forcedly positioned on a common axis, so that the mast will necessarily be rectilinear, thanks to the self-centering properties of the tapering terminal parts. With this type of coupling, the truncated cone-shaped “female” terminal part of each module must be free from protrusions preventing the insertion of the “male” terminal part of the successive module, thus being completely open.

The “male” terminal part, instead, may be provided with a collar or a rib that stiffens and strengthens its wall in a direction perpendicular to it. Said reinforcing collar or rib is useful to stiffen the walls perpendicularly, in order to reduce their local instability. This phenomenon, which is typical of thin shell-like structures, constitutes one of the main causes of breakage of masts of sailboats and limiting it means increasing safety. The construction of the modules in this example follows, but not necessarily, the normal processes for the manufacture of products in composite material treated/cured in autoclave and requires the use of a mould in two parts divided longitudinally along one of the meridians of the module.

Each of the two halves of the mould, which is also called half-mould, reproduces in the negative one half of the outer surface of the module.

The two coupled half-moulds reproduce the entire outer surface of the module. Both half-moulds are provided with flanges for reciprocal coupling.

Layers of fibres impregnated with resin are laid inside the grooves in the mould of the object to be obtained, properly treated in order to facilitate the detachment of said fibres. In one of the half-moulds the layers of fibres and resin are laid up to the edge for coupling with the other half-mould, while in the opposite half-mould the layers of fibres and resin project beyond said coupling edge.

A tubular bag preferably, but not necessarily, open at both ends is placed in this half-mould with projecting layers, on top of the layers of fibres and resin and inside the form to be obtained. The open ends of said tubular bag are arranged so that they come out of the terminal holes present in the mould. The diameter of each tubular bag is equal to or greater than the maximum diameter of the internal sections of the module, in such a way as to ensure the total filling of the hollow internal volume.

The projecting part of said layers of fibre and resin is folded and laid on top of said tubular bag.

The two half-moulds are joined together and the whole mould is enclosed in an external bag to which the free ends of the tubular bag positioned inside the mould are joined with a special sealing agent.

In this way the tubular bag and the external bag form a continuous closed nylon bag, inside which there is the mould with the fibres and the resin to be polymerised. According to a possible variant, a single tubular bag may be used, whose diameter exceeds the maximum external lateral length of the mould and whose length is more than twice the length of the mould. This bag is partially inserted in the mould as described above, and more than half of the bag is made project from one of the terminal holes of the mould. The projecting part is turned inside out, after the mould has been closed, in such a way as to cover the outer surface of the mould itself. At the end of this operation, the two terminal openings of the bag will be overlapped right out of one of the mould openings and therefore it will be possible to join and seal them together.

This variant allows one single sealing operation to be carried out on the bag, instead of two sealing operations, but in this case the bag must be handled much more, which results in an increased risk of breaking the bag itself.

The closed volume created by the bags is placed under vacuum by means of a suction pump that is connected in a suitable position along the outer surface of the mould and creates vacuum inside it, compressing the internal bag against the layers of fibre, which in turn are compressed against the internal wall of the mould.

The assembly of the two half-moulds joined in this way and contained in the bag is then placed in an autoclave, where the pressure at which the layers are compressed is increased, typically up to 6-7 bars.

In particular, the projecting part of the layers of fibre and resin laid in one of the half-moulds is compressed onto the layers of fibre and resin laid in the other half-mould, so as to obtain a continuous join between the layers of fibre and resin of the two half-moulds. The pump connected to the bag extracts both the air present inside the bag and the air that may have been trapped between the layers of fibre and resin or between said layers and the inside of the half-moulds during lamination.

It is possible to use half-moulds with coupling edges that can be sealed together, so as to avoid the use of the external bag, by sealing the internal bag against the outer walls of the mould. This solution, though requiring the construction of more complex moulds, ensures time and cost savings during production.

At the end of the polymerisation process, after the pumps have been switched off and the moulds opened, the module is drawn out of the moulds.

The module obtained has no joining lines, the layers of fibre and resin corresponding to the two half-moulds are perfectly joined and compressed along the entire internal surface, and the external surface of the module has no visible joins.

All the modules necessary to obtain the complete mast can be produced using the process chosen, independently of whether they are equal to or different from one another. In the latter case, different moulds must be used or, alternatively, removable inserts must be positioned in the moulds, so that modules with different characteristics can be obtained. In any case, each module must have one (if the module is going to make up one of the two ends of the mast) or two truncated cone-shaped terminal parts, which must be compatible with the terminal parts of the adjacent module. In order to allow the mast to be obtained by joining the modules with a single operation, the taper of each terminal part must be identical, so as to ensure the same pressure on each coupling surface.

Once all the necessary modules have been obtained, their coupling surfaces must be properly treated for the glueing operation, eliminating any impurities and chemical compounds that may prevent perfect adhesion. This treatment is often carried out through surface abrasion.

At this point all the modules should be aligned, bringing the truncated cone-shaped terminal parts close to one another, however without coupling them. In this phase the traction cable or rod may easily be inserted, making it pass from one module to the other, without applying any tension.

Successively, the adhesive is applied to both surfaces of each terminal part to be glued and the terminals are first coupled manually, by fitting them one into the other. Once all the terminal parts have been inserted, the threaded part of the inner cable or rod is passed through the central holes of two plates that must rest on the mast ends and at this point it is possible to start tensioning the cable with two nuts.

The pressure exerted on the coupling surfaces must be sufficient to eliminate any excess adhesive and air bubbles and to ensure that the thickness of the adhesive is as indicated by its manufacturer. The correct pressure is usually suggested by the manufacturer of the adhesive used.

Common trigonometric equations make it possible to calculate the exact cable tension necessary to obtain the required pressure on the surfaces to be glued. The common formulas for threaded couplings, instead, make it possible to calculate the driving torque that must be applied to the nuts to obtain the required tension.

The application of the calculated tension allow the modules to be strongly pressed against one another. The taper of the terminal parts will also impose the alignment of the modules along the longitudinal axis of the mast, thus ensuring its rectilinearity.

Finally, once the necessary pressure has been reached, the terminal parts can be heated up to the temperature necessary to treat/cure the adhesive. Therefore, there is no need to carry out complex temperature controls on a wide area, as would be necessary if two half-masts obtained from two open half-moulds were to be joined longitudinally, which is often the case in the production of boat masts in composite material.

BEST MODE FOR CARRYING OUT THE INVENTION

The characteristics of the new process for the production of modular hollow columns or rods, and the product obtained will be better explained by the following description with reference to the drawings, said drawings being enclosed purely as an example without limitation and referring to the production of modules in resin reinforced with fibres and polymerised at high pressure.

The following description refers to the production of a sailboat mast, but the considerations made apply to the production of any other rectilinear hollow object, generically tubular in shape and not necessarily made of resin reinforced with fibres and polymerised at high pressure.

FIG. 1 shows the two half-moulds (Sa, Sb) with the inside groove (S1) reproducing in the negative the external surface of a generic module.

Each half-mould (Sa, Sb) is provided with flanges or edges (S2) for coupling with the other half-mould (Sb, Sa).

The seat for the truncated cone-shaped terminal parts is visible on each one of the two half-moulds. At one end there is the male terminal part (S3), with the rib (S4) and the central opening (S5), while at the other end there is the female terminal part (S6), completely open towards the outside.

Both moulds (Sa, Sb) are covered with detaching agents, that is, products that falicitate the detachment of the object in fibre and resin made with the half-moulds (Sa, Sb) from the half-moulds themselves.

Layers of fibre and resin (M) are laid in the grooves (S1) of the two half-moulds (Sa, Sb), and are arranged so as to obtain the desired fibre thickness and layout on the walls of the object to be carried out.

In particular, in one half-mould (Sa) the layers of fibre and resin (M) are laid until reaching the surface of the half-mould (Sa) that is to be coupled with the complementary half-mould (Sb), while in the other half-mould (Sb) the layers of fibre and resin (M) are laid so that they project, in a suitable amount, beyond the coupling surface of the half-mould (Sb), as can be seen in the cross section shown in FIG. 2.

Successively, a tubular bag (G1) made of a plastic material resistant to high temperatures, typically polyamide or nylon, is placed inside the half-mould (Sb) with projecting layers of fibre and resin (M), said bag being open at both ends and said ends being arranged so that they protrude from the openings (S5, S6) present in the mould (Sb). Said tubular bag (G1) is cylindrical in shape and its diameter is equal to or greater than the maximum internal cross section of the object to be made and is positioned in such a way as to occupy all the space inside the object to be made.

FIG. 3 schematically represents the position of said tubular bag (G1).

The projecting part of the layers of fibre and resin (M) is laid on top of the tubular bag (G1) and the two half-moulds (Sa, Sb) are joined and closed together.

The mould (S), constituted by the two joined half-moulds (Sa, Sb), is enclosed into a tubular bag, hereinafter called external bag for the sake of simplicity, so that the two mouths of the tubular bag (G1), projecting from the openings (S5, S6) of the mould (S), are aligned with the mouths of the external bag.

Said mouths of the internal (G1) and external bag are joined and sealed with a special sealing agent.

One or more valves suitable for connection with a vacuum pump are positioned on the external bag.

The assembly made up of the mould (S) and of the internal (G1) and external bag is placed in an autoclave and the bags (G1, G2) are connected to a suction pump by means of said valves, thus extracting the air from the bag assembly (G1, G2).

Furthermore, the atmosphere of the autoclave acts on the bag (G1) inside the mould (S) and on the layers of fibre and resin (M), so that all the layers of fibre and resin (M) are compressed towards the walls of the inner groove (S1) of the two half-moulds (Sa, Sb). In particular said expansion of the internal bag (G1) involves also the compression of the projecting part of the layers of fibre and resin (M) laid in the half-mould (Sb) onto the layers of fibre and resin (M) of the other half-mould (Sa), in such a way as to obtain a continuous join between the layers of fibre and resin (M) of the two half-moulds (Sa, Sb). The suction pump extracts the air from the inside of the external bag. The air present inside the mould (S) and between the layers of fibre and resin (M) filters outside the mould (S) itself and is sucked by said suction pump.

Instead of an internal bag (G1) initially separated from the external bag and successively joined to it by means of a special sealing agent applied to both ends, as described above, it is possible to use a single bag (G), with cross section sufficient to completely surround the outside of the mould (S) and length more than twice the length of the mould (S). In this case, approximately one half of this bag (G) would be introduced in the half-mould (Sb), in the same way described for the internal bag (G1), letting the other end protrude from one of the two openings (S5 or S6) of the mould (S). Once the two half-moulds (Sa, Sb) have been joined and closed, the protruding part of the bag (G) would be turned inside out, in such a way as to cover the outside of the mould (S). In this case, there is only one end of the bag to be sealed, the other end being constituted by a fold of the bag (G) itself. As to the other aspects, the method is equivalent to the one already proposed. An equivalent solution involves the use of half-moulds (Sa, Sb) that can be sealed together so as to avoid the use of the external bag. The internal bag (G1) that comes out of the two ends (S5, S6) of the mould (S) is widened and its edges are sealed around the openings of the mould (S5, S6).

The two half-moulds (Sa, Sb) are sealed along their joining line, so as to create a closed chamber coinciding with the mould (S), and the air is sucked out of the mould (S), by connecting the pump to one or both the protruding ends of the internal bag (G1). Said second solution, though maintaining the internal bag (G1), avoids the use of the external bag.

The layers of fibre and resin (M) laid in the two half-moulds (Sa, Sb) will be perfectly joined and compressed along their entire internal surface.

The internal bag (G1) ensures the compression and the adhesion between the various layers of fibre and resin (M), as well as between the edges of the layers (M) of a half-mould (Sa) and the edges of the layers (M) of the complementary half-mould (Sb). The construction method described above uses already known technologies for the manufacture of products in composite materials with treatment/curing of the resin in autoclave and makes it possible to obtain a module having the best structural characteristics obtainable with composite materials in resin reinforced with fibres. This process must be repeated for a number of times corresponding to the number of modules necessary to obtain the desired mast.

The single modules, however, can also be carried out with technologies different from the one described, for example they can be produced using the method known as filament-winding, or through manual impregnation of the fibres, or using thermoplastic instead of thermosetting resins. The polymerisation of the resin can be carried out with or without application of pressure. The polymerisation can be obtained at temperatures different from the one indicated and even without using the bag under vacuum.

The modules needn't be produced with the same mould (S), in fact different moulds can be used to make, for example, the base or top module of the mast, or any module provided with couplings for the mast support cables or for the sailing equipment, as shown in FIG. 1. The application of the invention described herein allows a wide range of different features of the single modules to be obtained. The only condition to be respected is that all modules must be provided with truncated cone-shaped terminal parts (S3, S6), which are necessary for coupling them with the adjacent modules. The base module, if any, may be constructed with the top end only (S3) and the top module, if any, may be constructed with the bottom end only (S6).

After the modules necessary to make up the mast have been obtained with the processes described herein, their truncated cone-shaped terminal parts (S3, S6) must be prepared for glueing, following the procedures recommended for the adhesive used. On the “male” terminal parts (S3) the external surface must be prepared, while the internal surface must be prepared on the “female” terminal parts (S6).

After preparing the terminal parts (S3, S6) of each module for glueing, the modules must be aligned, for example by resting them on stands, in the established order, for example with the base module on one side, the top module on the opposite side and the intermediate modules in the middle, with any modules provided with couplings for the support cables or for the sailing equipment in the positions required by the structure of the mast to be carried out.

FIG. 4 shows, by way of example only, a possible alignment with a base module (R3), provided with the male terminal part (S3) only, two equal modules (R1), each provided with a male terminal part (S3) and a female terminal part (S6), and a module provided with couplings for the mast support cables (R2), with a female (S6) and a male terminal part (S3), not indicated in the figure as it is not utilized due to the absence of other modules to be joined.

With the modules aligned in the correct order, the adhesive must be applied to all the truncated cone-shaped terminal parts (S3, S6) and a traction cable or rod (A) will be made slide inside each module, the length of said traction cable or rod being sufficient to cover the entire inner cavity of the mast when the modules are adjacent to one another, but haven't been joined yet.

Said traction cable or rod (A) must be provided with a device suited to exert a controlled tension, by acting on the mast ends, which therefore will be compressed accordingly. A suitable device, proposed herein as a non-exclusive solution, is constituted by two threaded bars, applied to the ends of the cable, or by a thread on the whole rod or its ends. After making said traction cable or rod slide inside the series of aligned modules, the threaded ends must be passed through two plates (P1, P2), each one provided with a central hole and having dimensions sufficient to rest on the entire perimeter of the two ends of the mast, and/or being provided with seats specifically designed for this purpose. The plates, however, must be positioned in such a way as to transfer to the mast a compression force parallel to the longitudinal axis of the mast itself.

Successively the various modules can be brought in contact with one another by hand, inserting the “male” truncated cone-shaped terminal parts (S3) into the adjacent “female” terminal parts (S6) and compressing them towards one another as much as possible (FIG. 5).

Once the preliminary coupling of all the modules has been completed, two nuts must be inserted in the threaded ends of the traction cable or rod (A). Said nuts will be tightened against the two plates (P1, P2), thus increasing the tension of the traction cable or rod. Said tension can be easily controlled by adjusting the nut driving torque by means of a torque wrench.

The tension of the traction cable or rod is transferred, through the 2 plates (P1, P2), to the series of modules laid one after the other, acting as an axial compression on the mast. A possible variant to the use of the internal cable or rod is the use of a device external to the column, suitable for the application of a controlled axial compression to the column itself.

The taper of the terminal parts (S3, S6) makes the axial compression act on the coupling areas as a pressure perpendicular and radial to the walls. This pressure compresses the outside of the walls of the male terminal part (S3) against the inside of the walls of the female terminal part (S6).

If the taper is the same for all the truncated cone-shaped terminal parts, the pressure perpendicular to the walls will be the same on each coupling area. In this way, by assigning a suitable taper angle to the terminal parts, for example 2°, it is possible to calculate the mathematical relation between the axial compression applied to the mast by the traction cable or rod (A) and the pressure perpendicular and radial to the walls of the terminal parts.

The pressure between the walls to be glued is necessary to ensure: 1) the contact between the walls themselves and therefore between the fibres of the laminate, without interposition of excessively thick layers of glue; 2) the elimination of excess adhesive at the end of the coupling areas; 3) the elimination of any air bubbles present between the walls of the terminal parts; 4) the axial centering of the various modules. The points 1), 2) and 3) represent some of the fundamental factors to ensure that the connection of the parts by glueing achieves the best mechanical characteristics obtainable with the adhesive used. If these conditions are respected and if the adhesive used has sufficient mechanical characteristics, it is possible to ensure that the mechanical resistance of the glued terminal parts is equal to or higher than that of the connected modules.

The pressure suitable to achieve the aims 1), 2) and 3) must be verified with the manufacturer of the adhesive, but the invention described herein, through the control of the taper angle of the terminal parts of the modules (S3, S6) and of the nut driving torque, allows said pressure to be easily exerted by using the simple equipment described above. The use of the truncated cone-shaped terminal parts described herein also makes it possible to achieve the aim 4), with no need to make use of sophisticated supports to keep the modules perfectly aligned during glueing. Thanks to the taper of the terminal parts, the various modules align spontaneously along the axis of the mast, without any tendency to bend sidewards or vertically upwards.

It is sufficient to support the aligned modules with simple stands, or to rest them on the ground, to eliminate the effect of their dead load and ensure the rectilinear assembly of the mast.

Thanks to this property of the tapered terminal parts it is possible to avoid the use of any type of template or support for the correct assembly of the column and there is no need to check the alignment of separate elements of the column, which on the other hand is necessary if the elements are divided along a direction parallel to the axis of the column. After carrying out the coupling described herein and tightening the nuts with the calculated torque, it is possible to subject the adhesive to heat treatment, if required. For this purpose it isn't necessary to heat the whole mast, since the parts to be treated are only the terminal parts (S3, S6) between the modules. The scarce heat conductivity of the common resins and fibres used in the manufacture of composite materials limits the dispersion of the heat applied to the terminal parts and therefore also the energy necessary to achieve the required temperature.

To increase the temperature of the terminal parts during the treatment/curing of the adhesive it is possible, among other methods, to use heating blankets, if necessary wrapping the terminal parts with layers of heat insulating material.

Therefore, with reference to the above description and the enclosed drawings, the following claims are expressed. 

1. Process for the production of a hollow structural column or rod in polymers, obtained by assembling modules having shorter length, characterized in that it comprises two or more elongated modules, each one provided with male-female truncated cone-shaped terminal parts, wherein the inner surface of the “female” terminal part has a taper angle that is identical to the taper angle of the outer surface of the “male” terminal part, and the following steps: aligning said hollow modules; preparing said male and female terminal parts with adhesive for glueing and insertion in the terminal part of the adjacent, aligned module; applying, preferably at the ends, an axial compression device, so that on compression of the ends of the rod made up of said modules each external male tapering surface adheres to and exerts a suitable pressure on the internal female tapering surface of the adjacent module during the structural joining and glueing of the terminal parts and the polymerisation of the adhesive.
 2. Process for the production of a hollow structural column or rod in polymers according to claim 1, characterized in that the overlapping areas of the male and female tapering terminal parts are sufficiently wide to ensure that the glue or structural adhesive is capable of transferring the project loads.
 3. Process for the production of a hollow structural column or rod in polymers according to claims 1, 2, characterized in that the taper of the terminal parts converts the axial compression on the column into a local pressure perpendicular or radial in relation to the walls of the terminal parts.
 4. Process for the production of a modular hollow structural column or rod in polymers according to claims 1, 2, 3, characterized in that the taper of the terminal parts ensures the spontaneous alignment of the modules during the assembly and glueing steps.
 5. Process for the production of a hollow structural column or rod in polymers according to claims 1, 2, 3, 4, characterized in that the male terminal part is provided with an orthogonal wall or partition that serves as local reinforcement suited to limit the instability of the walls.
 6. Process for the production of a modular hollow structural column or rod in polymers according to the previous claims, characterized in that said modules are provided with openings at both ends for the passage of the axial compression device.
 7. Process for the production of a modular hollow structural column or rod in polymers according to claims 1, 2, 3, 4, 5, 6, characterized in that the compression device comprises a rod passing in axial position through all said modules and provided with plates or coupling elements at the ends of the first and last module.
 8. Process for the production of a modular hollow structural column or rod in polymers according to claim 7, characterized in that the traction device allows the tension applied to the device to be controlled.
 9. Process for the production of a modular hollow structural column or rod according to the previous claims, characterized in that the compression device is external to the rod or column.
 10. Process for the production of a modular hollow structural column or rod according to the previous claims, characterized in that some modules can be provided with cross elements, couplings, supports, connections, branches, etc.
 11. Process for the production of a modular hollow structural column or rod according to the previous claims, characterized in that one or more modules are provided with a tight cavity.
 12. Process for the production of a modular hollow structural column or rod according to the previous claims, characterized in that said polymers are integrated with fibres of any suitable type, like carbon fibres, glass fibres, aramidic fibres, boron fibres or fibres of other metals or ceramic fibres.
 13. Structural hollow rod or column in polymers, characterized in that it is constructed by assembling modules with shorter length, and in that it comprises two or more aligned hollow modules, elongated in shape, each one provided with male-female truncated cone-shaped terminal parts, treated with adhesive, and wherein the inner surface of the “female” terminal part has a taper angle that is identical to that of the outer surface of the “male” terminal part, and wherein an axial compression device, positioned between the rod ends, exerts a suitable pressure on the contact surfaces between the modules during the structural joining and glueing of the terminals and the polymerisation of the adhesive. 